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Other Designations: Inflatable Antenna Experiment. Class: Technology. Destination: Maximum Payload Orbit. Nation: USA. Agency: NASA/JPL. Deployed from Spartan 207 5/20/96; test of inflatable antenna technology. Reentered May 22. Typical orbit: 190 km circular orbit, 39 deg inclination.
IAE Chronology - 1996 May 19 - IAE - Launch Site: Cape Canaveral. Launch Complex: LC39B. Launch Vehicle: Shuttle. Perigee: 180 km (110 mi). Apogee: 201 km (124 mi). Inclination: 39.10 deg. Period: 88.30 min.
LEO. Inflatable Antenna Experiment; deployed from Spartan 207 5/20/96; test of inflatable antenna technology. Reentered May 22.
Bibliography:- McDowell, Jonathan, Jonathan's Space Home Page (launch records), Harvard University, 1997-present. Web Address when accessed: http://www.planet4589.org/jsr.html.
- McDowell, Jonathan, Jonathan's Space Report (Internet Newsletter), Harvard University, Weekly, 1989 to Present. Web Address when accessed: http://www.planet4589.org/jsr.html.
- JPL Mission and Spacecraft Library, Jet Propulsion Laboratory, 1997. Web Address when accessed: http://msl.jpl.nasa.gov/home.html.
- NASA GSFC Orbital Parameters,
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